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Computational Investigation of Nominally-Orthogonal Pneumatic Active Flow Control for Aircraft High-Lift SystemsNo abstract available
Document ID
20180001230
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Hosseini, S. Sheida (Science and Technology Corp. Moffett Field, CA, United States)
van Dam, C. P. (California Univ. Davis, CA, United States)
Pandya, Shishir (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
February 15, 2018
Publication Date
January 9, 2018
Subject Category
Aerodynamics
Aircraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN51287
Meeting Information
Meeting: AIAA SciTech Forum
Location: Kissimmee, FL
Country: United States
Start Date: January 8, 2018
End Date: January 12, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA16BD60C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Fluidic
Nominally-Orthogonal
High-Lif

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